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gptkbp:instanceOf
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gptkb:helicopter
|
|
gptkbp:armament
|
none
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gptkbp:avionics
|
modern avionics suite
|
|
gptkbp:cockpit
|
glass cockpit
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:USA
gptkb:Sikorsky_Aircraft_Corporation
high maneuverability
|
|
gptkbp:developer
|
gptkb:Sikorsky_Aircraft_Corporation
|
|
gptkbp:electrification
|
1 × Allison 250-C20B
|
|
gptkbp:emergencyServices
|
floatation gear
|
|
gptkbp:engine
|
gptkb:Allison_250-C20B
|
|
gptkbp:engineType
|
turboshaft
|
|
gptkbp:firstFlight
|
1990
|
|
gptkbp:fuelCapacity
|
600 L
|
|
gptkbp:headlights
|
gptkb:fenestron
2
|
|
gptkbp:height
|
4.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Sikorsky S-300U
|
|
gptkbp:introduced
|
1990
|
|
gptkbp:landingGear
|
skids
|
|
gptkbp:length
|
15.5 m
|
|
gptkbp:manufacturer
|
gptkb:Sikorsky_Aircraft_Corporation
|
|
gptkbp:market
|
global
|
|
gptkbp:marketSegment
|
military and civilian
|
|
gptkbp:maximumDepth
|
1,400 kg
|
|
gptkbp:maxSpeed
|
250 km/h
|
|
gptkbp:maxTakeoffWeight
|
3,200 kg
3,600 kg
|
|
gptkbp:militaryRank
|
yes
|
|
gptkbp:notableFeature
|
1991
4
|
|
gptkbp:notableUsers
|
gptkb:United_States_Army
|
|
gptkbp:numberBuilt
|
over 100
|
|
gptkbp:operationalHistory
|
used in various countries
|
|
gptkbp:operationalRange
|
500 km
|
|
gptkbp:passengerCapacity
|
6
optional
|
|
gptkbp:primaryUser
|
military
|
|
gptkbp:productionYears
|
1990-2000
|
|
gptkbp:products
|
FAA_certified
|
|
gptkbp:range
|
600 km
|
|
gptkbp:role
|
utility helicopter
training helicopter
|
|
gptkbp:rotorDiameter
|
13.4 m
|
|
gptkbp:safetyFeatures
|
dual controls
|
|
gptkbp:services
|
3,000 m
|
|
gptkbp:setting
|
single rotor
|
|
gptkbp:status
|
in production
|
|
gptkbp:successor
|
gptkb:Sikorsky_S-400
|
|
gptkbp:supportRole
|
pilot training
|
|
gptkbp:variant
|
gptkb:Sikorsky_S-300_series
|
|
gptkbp:weight
|
2,200 kg
|